What was found
AT C-CHECK, LEFT WING VERTICAL STIFFENER CRACKED AT LOWER END ON FWD SPAR WEB. STOP DRILLED CRACK, HFEC, INSTALLED ANGLE REPAIR PER SRM 51-40-3, 1.125 X 1.125 X 6.5. N/R 1124
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AT C-CHECK, LEFT WING VERTICAL STIFFENER CRACKED AT LOWER END ON FWD SPAR WEB. STOP DRILLED CRACK, HFEC, INSTALLED ANGLE REPAIR PER SRM 51-40-3, 1.125 X 1.125 X 6.5. N/R 1124